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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

500°C
700°C
1000°C
200°C

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Compressors, Gas Turbines and Jet Engines
An air compressor may be controlled by

Throttle control
Blow off control
Any one of the above
Clearance control

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Compressors, Gas Turbines and Jet Engines
The work-done on a compressor will be minimum if air is taken from

The atmosphere
A source at 0° C
A source of high temperature air
A source of low temperature air

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Compressor
Heating chamber
Cooling chamber
All of these

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Cools the delivered air
Is the standard practice for big compressors
Results in saving of power in compressing a given volume to given pressure
Enables compression in two stages

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Compressors, Gas Turbines and Jet Engines
A simple turbojet engine is basically

Gas turbine engine equipped with a propulsive nozzle and diffuse
Chemical rocket engine
Ramjet engine
A propeller system

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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